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2 edition of Theoretical and experimental methods in hypersonic flows found in the catalog.

Theoretical and experimental methods in hypersonic flows

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.

Theoretical and experimental methods in hypersonic flows

papers presented and discussions held at the Fluid Dynamics Panel Symposium held in Torino, Italy, from 4th-8th May 1992.

by North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.

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  • 35 Currently reading

Published by AGARD in Neuilly-sur-Seine .
Written in English


Edition Notes

SeriesAGARD conference proceedings -- 514
The Physical Object
Pagination1 v. (various pagings) :
ID Numbers
Open LibraryOL20251452M
ISBN 109283506944

Existing DSMC reaction models accurately reproduce experimental equilibrium reaction rates, but the applicability of these rates to the strong thermal nonequilibrium observed in hypersonic shocks is unknown. For re-entry flows, these modeling issues are particularly relevant for Cited by: 4.


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Theoretical and experimental methods in hypersonic flows by North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Download PDF EPUB FB2

Abstract: Major topics covered by the Symposium were testing techniques and instrumentation, computational methods and physical modeling, and validation and accuracy assessment. The sessions were: (1) Design of Hypersonic Vehicle; (2) Facilities;(3) Instrumentation; (4) CFD Validation and Data Accuracy; (5) Rarefied Gas; Real Gas; Chemistry; (6) Boundary Layer Transition; (7) High Enthalpy.

The subjects can be grouped into the following areas: Phys­ ical environments, configuration requirements, propulsion systems (including airbreathing systems), experimental methods for external and internal flow, theoretical and numerical by: Get this from a library.

Theoretical and experimental methods in hypersonic flows = Les méthodes théoriques et expérimentales pour l'etude des ecoulements hypersoniques. [North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel.

Symposium; North Atlantic Treaty Organization. Molecular Physics and Hypersonic Flows bridges the gap between the fluid dynamics and molecular physics communities, emphasizing the role played by elementary processes in hypersonic flows.

In particular, the work is primarily dedicated to filling the gap between microscopic and macroscopic. The main idea of these Courses was to present to chemists, com­ puter scientists, engineers, experimentalists, mathematicians, and physicists state of the art lectures in scientific and technical dis­ ciplines including mathematical modeling, computational methods, and experimental measurements necessary to define the aerothermo­ dynamic environments for space vehicles such as the US Orbiter or the European Hermes flying at hypersonic speeds.

Chapter 5, on hypersonic flows, covers the physics of hypersonic flows systematically. Newtonian flow model and Mach number independence principles are discussed to the : Ethirajan Rathakrishnan. Hypersonic Flow Theory presents the fundamentals of fluid mechanics, focusing on the hypersonic flow theory and approaches in theoretical aerodynamics.

This book discusses the assumptions underlying hypersonic flow theory, unified supersonic-hypersonic similitude, two-dimensional and axisymmetric bodies, and circular cylinder.

Ten chapters address: general characterization of hypersonic flows; basic equations of motion; defining the aerothermodynamic environment; experimental measurements of hypersonic flows; stagnation-region flowfield; the pressure distribution; the boundary layer and convective heat transfer; aerodynamic forces and moments; viscous interactions; and aerothermodynamics and design.

Progress in Astronautics and Rocketry, Volume 7: Hypersonic Flow Research compiles papers presented at a conference on hypersonics held at the Massachusetts Institute of Technology in August This book discusses the low Reynolds number effects, chemical kinetics effects, inviscid flow calculations, and experimental techniques relating to Book Edition: 1.

Comprehensive results of a joint experimental and computational study of the two-dimensional flow field over flat plate/compression ramp configurations at Mach 14 are presented. These geometries are aimed to simulate, in a simplified manner, the region around deflected control surfaces of hypersonic re-entry by:   An effective experimental method and apparatus for unsteady water vapor condensation investigation in high speed expansion flow Review of Scientific Instruments, Vol.

90, No. 6 Numerical Study of Unsteady High Enthalpy Flow in an Expansion TubeCited by: Introduction to Hypersonic Flows. (including airbreathing systems), experimental methods for external and internal flow, theoretical and numerical methods. Since hyper­ sonic flight requires.

In the hypersonic regime the scramjet engine's specific thrust exceeds that of other propulsion systems. This book, written by a leading researcher, describes the processes and characteristics of the scramjet engine in a unified manner, reviewing both the theoretical and experimental research.

Springer, p. This book is intended as a text for undergraduate and graduate courses in aerodynamics, typically offered to students of aerospace and mechanical engineering programs. It covers all aspects of aerodynamics. The book begins with a description of the standard atmosphere and. Developing a new aircraft several theoretical and experimental researches must be performed in order to avoid noxious aeroelastic phenomena during the later use of the aircraft.

hypersonic flow fields can be grouped in two major categories: the fields where the flows can be considered everywhere to be in thermodynamic equilibrium, and the.

A theoretical model of an elastic panel in hypersonic flow is derived to be used for design and analysis. The nonlinear von Kármán plate equations are coupled with 1st order Piston Theory and linearized at the nonlinear steady-state deformation due to static pressure differential and thermal : Maxim Freydin, Earl H.

Dowell, Thomas J. Whalen, Stuart J. Laurence. Theoretical and experimental study of rarefied supersonic flows about several simple shapes. "Theoretical and experimental study of rarefied supersonic flows about several simple shapes." AIAA Journal, Vol. 6, No. 12 Numerical Simulation of Hypersonic Rarefied Flows Using the Second-Order Constitutive Model of the Boltzmann Equation Cited by: This workshop has been organized in close connection with the AGARD FDP Symposium to be held in Torino 4 - 8 May on "Theoretical and Experimental Methods in Hypersonic Flows": the main conclusions and ideas expressed by the papers and during the discussions of this workshop are reported in session 7 and have been presented in Torino in a Format: Paperback.

The High Temperature Aspects of Hypersonic Flow is a record of the proceedings of the AGARD-NATO Specialists' Meeting, held at the Technical Centre for Experimental Aerodynamics, Rhode-Saint-Genese, Belgium in April The book contains the papers presented during the meeting that tackled a broad range of topics in the aspects of hypersonic Book Edition: 1.

This paper discusses the experimental study of the effect of sweep on the aerodynamic characteristics of thin slab delta wings with flaps at hypersonic speeds. For the purpose of this investigation, a novel Cited by: 4. The requirement of the design process of hypersonic vehicles to predict flow past entire configurations with wings, fins, flaps, and propulsion system represents one of the major challenges for aerothermodynamics.

In this context computational fluid dynamics has come up as a powerful tool to support the experimental work.

A couple of numerical methods developed at MBB designed to fulfill Cited by: 3. Supersonic and Hypersonic Flows. Several experimental and theoretical/numerical works have been conducted to explore this flow; however, there is a dearth of literature detailing the instantaneous flow which is vital to improve the efficiency of the mixing of fluids.

Birch, Computational Fluid Dynamics Methods for Hypersonic Flow. Theoretical and Experimental Aerodynamics Mrinal Kaushik This book is intended as a text for undergraduate and graduate courses in aerodynamics, typically offered to students of aerospace and mechanical engineering programs.

Description. Results of theoretical and experimental studies of the problems concerned super/hypersonic flows around the models of real space vehicle configurations such as "Buran"-orbiter, winged cone (airplane-like body), Clipper space vehicle, Martian planetary probe are presented.

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Whether you've loved the book or not, if you give your honest and detailed thoughts then people will find new books that are right for them. Recent Advances in Theoretical, Applied, Computational and Experimental Mechanics by B. Singh,available at Book Depository with free delivery worldwide.

Methods for Turbulent Reacting Flow Calculations Basic Methods. Hybrid PDF/FDF‐Methods. Some Deficiencies of Existing Hybrid PDF‐Methods The Transport Problem.

The Mixing Problem. The Energy Problem. New Theoretical Concepts The Transport Problem. The Mixing Problem. surement. How should experimental data be analyzed to generate practical information. Although the main focus of the book is food, scientists and engineers in other fields will find the work a convenient reference for standard rheological methods and typical data.

Overall, the work presents the theory of rheological testing and. Get this from a library. Advances in Hypersonics: Computing Hypersonic Flows Volume 3. [John J Bertin; Jacques Périaux; Josef Ballmann] -- These three volumes entitled Advances in Hypersonics contain the Proceedings of the Second and Third Joint US/Europe Short Course in Hypersonics which took place in Colorado Springs and Aachen.

The. Audio Books & Poetry Community Audio Computers, DTIC AD COMPARISON OF THEORETICAL AND EXPERIMENTAL PRESSURE AND HEAT-TRANSFER DISTRIBUTIONS ON THREE BLUNT NOSED CYLINDERS IN HYPERSONIC FLOW Item Preview.

Theoretical, Experimental, and Numerical Contributions to the Mechanics of Fluids and Solids, () Hypersonic aerodynamics on thin bodies with interaction and upstream influence.

Journal of Fluid Mechanics 1, Cited by: The main objective of this research is to develop a hybrid particle/continuum numerical method for simulating hypersonic interaction flows.

This method is expected to be physically more accurate and numerically more efficient than a conventional method that simply employs either particle or continuum approach, but not both.

NUMERICAL AND EXPERIMENTAL STUDIES OF SHOCK INTERFERENCE IN HYPERSONIC FLOWS NEAR A CYLINDER 3 Experimental Techniques and Results The experiments have been carried out in a vacuum wind tunnel at low-density uniform airflow parameters: M¥ =T 0 = K, p 0 = a N/m2, and t w = The model is a plate.

Download Defining The Hypersonic Environment ebook PDF or Read Online Click Download or Read Online button to Defining The Hypersonic Environment book pdf for free now. Hypersonics. Author: BERTIN ISBN: X Genre: Science File Size: MB experimental methods for external and internal flow, theoretical and numerical.

Book Title: Theoretical and Experimental Aerodynamics: Author: Mrinal Kaushik: Publisher: Springer: Release Date: flow analogies and hypersonic (rotational) flows.

A unique feature of the book is its ten self-tests and their solutions as well as an appendix on special techniques of functions of complex variables, method of.

Characteristics of flow. While the definition of hypersonic flow can be quite vague and is generally debatable (especially due to the absence of discontinuity between supersonic and hypersonic flows), a hypersonic flow may be characterized by certain physical phenomena that can no longer be analytically discounted as in supersonic flow.

Existing DSMC reaction models accurately reproduce experimental equilibrium reaction rates, but the applicability of these rates to the strong thermal nonequilibrium observed in hypersonic shocks is unknown.

For hypersonic flows, these modeling issues are particularly relevant for nitrogen, the dominant species of air. Publications: Application of the Hodograph Method to Transonic Flows with Shocks, M.

Holt and J. Chattot, Proc. 3rd International Conference of Numerical Methods in Fluid Dynamics, er-Verlag,Lecture Notes in Physics, Transonic Flows with Shock Waves: Review of the Methods for Computing flows of Perfect Fluids Past Profiles, J.

Chattot, D. Guiraud, and P. Laval. @article{osti_, title = {STAGNATION-POINT HEAT TRANSFER MEASUREMENTS IN HYPERSONIC, LOW-DENSITY FLOW. Paper 7 of GENERAL RESEARCH IN FLIGHT SCIENCES, JANUARY JANUARY VOLUME I. FLUID MECHANICS. PART 2}, author = {Neice, S E and Rutowski, R W and Chan, J K}, abstractNote = {An experimental investigation of the heat-transfer.

Computational fluid dynamics (CFD) is the important tool to analyze physics of fluids. Hypersonic flows over real space configurations represent a substantial problem from the point of view of the development of new and more effective mathematical models, numerical methods, and the use of computer systems.

Governing equations for multi-component, multi-temperature, chemically reacting non Author: Yuriy D. Shevelev. Hypersonic Aerodynamics Introduction Hypersonic vehicles are commonplace. There are many more of them than the supersonic aircraft discussed in the last chapter.

Applications include missiles, launch vehicles and entry bodies. A huge effort has been made developing hypersonic aerodynamics methods and Size: 1MB.A magnetohydrodynamic drive or MHD accelerator is a method for propelling vehicles using only electric and magnetic fields with no moving parts, accelerating an electrically conductive propellant (liquid or gas) with fluid is directed to the rear and as a reaction, the vehicle accelerates forward.

The first studies examining MHD in the field of marine propulsion date.The purpose of this investigation was to initiate an experimental data base for Mach 5 cruise aircraft concepts.

A second objective was to compare appro- priate analysis methods with the test data. Hypersonic impact theory and super- sonic linearized theory were chosen for the comparison since both could be effective between Mach 3 and Mach Size: 6MB.